View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53134U 26145.38067029 +.00000000 +00000-0 -10272-3 0 00008
2 53134 53.2119 189.8413 0001587 61.0643 299.0508 15.08848780 06
| Epoch (UTC): | 25 May 2026 09:08:09 |
| Eccentricity: | 0.0001587 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.8413° |
| argument of perigee: | 61.0643° |
| revolutions per day: | 15.08848780 |
| mean anomaly at epoch: | 299.0508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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